A quantitative optimisation model for a horizontal MEMS solid propellant thruster with experimental verification

Qiang Shen; Weizheng Yuan; Jianbing Xie; Honglong Chang

doi:10.1007/s00542-015-2486-7

A quantitative optimisation model for a horizontal MEMS solid propellant thruster with experimental verification

Qiang Shen, Weizheng Yuan, Jianbing Xie, Honglong Chang

机电学院

Northwestern Polytechnical University Xian

科研成果: 期刊稿件 › 文章 › 同行评审

8 引用（Scopus）

摘要

This paper studies the effect of multiple geometric parameters of a micronozzle on a MEMS solid propellant thruster (MSPT) and establishes a quantitative optimisation model. Influences of the structural parameters of the micronozzle on performance are accurately calculated. The significance and contribution ratio of each parameter are evaluated by F distribution. Correspondingly, a horizontal MSPT is fabricated and tested to prove the optimisation model. In the implementation, a complete microigniter is formed by a single layer of Au, achieving an ultra-low ignition voltage of 2.1 V with an extremely low ignition resistance of 4 Ω.

源语言	英语
页（从-至）	847-859
页数	13
期刊	Microsystem Technologies
卷	22
期	4
DOI	https://doi.org/10.1007/s00542-015-2486-7
出版状态	已出版 - 1 4月 2016

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abstract = "This paper studies the effect of multiple geometric parameters of a micronozzle on a MEMS solid propellant thruster (MSPT) and establishes a quantitative optimisation model. Influences of the structural parameters of the micronozzle on performance are accurately calculated. The significance and contribution ratio of each parameter are evaluated by F distribution. Correspondingly, a horizontal MSPT is fabricated and tested to prove the optimisation model. In the implementation, a complete microigniter is formed by a single layer of Au, achieving an ultra-low ignition voltage of 2.1 V with an extremely low ignition resistance of 4 Ω.",

author = "Qiang Shen and Weizheng Yuan and Jianbing Xie and Honglong Chang",

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AU - Shen, Qiang

AU - Yuan, Weizheng

AU - Xie, Jianbing

AU - Chang, Honglong

PY - 2016/4/1

Y1 - 2016/4/1

N2 - This paper studies the effect of multiple geometric parameters of a micronozzle on a MEMS solid propellant thruster (MSPT) and establishes a quantitative optimisation model. Influences of the structural parameters of the micronozzle on performance are accurately calculated. The significance and contribution ratio of each parameter are evaluated by F distribution. Correspondingly, a horizontal MSPT is fabricated and tested to prove the optimisation model. In the implementation, a complete microigniter is formed by a single layer of Au, achieving an ultra-low ignition voltage of 2.1 V with an extremely low ignition resistance of 4 Ω.

AB - This paper studies the effect of multiple geometric parameters of a micronozzle on a MEMS solid propellant thruster (MSPT) and establishes a quantitative optimisation model. Influences of the structural parameters of the micronozzle on performance are accurately calculated. The significance and contribution ratio of each parameter are evaluated by F distribution. Correspondingly, a horizontal MSPT is fabricated and tested to prove the optimisation model. In the implementation, a complete microigniter is formed by a single layer of Au, achieving an ultra-low ignition voltage of 2.1 V with an extremely low ignition resistance of 4 Ω.

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A quantitative optimisation model for a horizontal MEMS solid propellant thruster with experimental verification

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